A system for thermal management and structural containment includes an enclosure, a heat source disposed within the enclosure; and a wick encompassing at least a portion of an outer surface of the heat source.
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1. A system for thermal management and structural containment, comprising:
an enclosure;
at least one battery disposed within the enclosure;
a battery surface wick encompassing at least a portion of an outer surface of the at least one battery;
an interior base wick disposed on and in thermal communication with an inner surface of a first wall of the enclosure, wherein the interior base wick is in capillary force communication with the battery surface wick;
and
a working fluid in capillary force communication with the battery surface wick.
2. The system of
an interior wick structure disposed on and in thermal communication with an interior surface of a second wall of the enclosure, wherein the interior wick structure is in capillary force communication with the interior base wick.
3. The system of
a heater disposed on an exterior side of a second wall, the heater disposed in complementary opposition to the interior wick structure.
4. The system of
wherein a portion of an outer surface of each battery of the first plurality of batteries is encompassed by a battery surface wick, and
wherein the battery surface wick of each battery of the first plurality of batteries is in capillary force communication with the interior base wick.
5. The system of
6. The system of
7. The system of
a second plurality of batteries stacked in a mono-block configuration on the interior base wick, wherein each battery of the second plurality of batteries comprises an outer surface encompassed by a battery surface wick, and
wherein the battery surface wick of each battery of the second plurality of batteries is in capillary force communication with the interior base wick.
8. The system of
an interior frame structure between the first plurality of batteries and the second plurality of batteries.
10. The system of
11. The system of
evaporation of a portion of the working fluid from the battery surface wick upon receiving heat from the at least one battery;
condensation of at least a portion of the evaporated portion of the working fluid on the interior base wick; and
fluid transportation by a capillary force of the condensed evaporated portion of the working fluid from the interior base wick to the battery surface wick.
12. The system of
13. The system of
14. The system of
15. The system of
16. The system of
19. The system of
20. The system of
21. The system of
evaporation of a portion of the working fluid from the battery surface wick upon receiving heat from the at least one battery;
condensation of a portion of the evaporated portion of the working fluid on the interior wick structure; and
fluid transportation by a capillary force of the condensed evaporated portion of the working fluid from the interior wick structure to the battery surface wick via the interior base wick.
22. The system of
evaporation of a portion of the working fluid from the interior wick structure upon receiving heat from the heater; and
condensation of a portion of the evaporated portion of the working fluid on the battery surface wick.
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This invention relates to phase-change cooling systems, and more particularly phase-change systems that use a wick.
Li-ion battery arrays are subject to lower than desired lifetime, are subject to reliability issues and may experience catastrophic failure due to excess heat build-up during certain charge and discharge operations. These concerns may be addressed by providing for excess battery capacity to reduce the charge/discharge rate for any particular one battery in the array. The arrays may also be actively cooled to reduce cell case temperature. For example, air or electrically non-conductive liquid may be circulated around the array to transport excess heat away from the array. Alternatively, a phase change material may be provided around the array to absorb excess heat. Several layer of safety features are generally required to provide fail-safe systems.
A need still exists to provide for improved thermal management and physical safety features for batteries and other heat sources.
A system for thermal management and structural containment may include an enclosure, a heat source disposed within the enclosure and a wick encompassing at least a portion of an outer surface of the heat source. The system may also include a working fluid disposed within the enclosure and that is in communication with the wick. The enclosure may be substantially vapor tight. The wick may include a material selected from the group consisting of ceramic, cellulose, glass, graphite, or polymer fibers, and may include a fabric selected from the group consisting of non-woven, woven, knitted, or braided fibers. The wick may be a multiscale wick, and may have a plurality of wick layers, each adjacent layer having a different pore size distribution. In one embodiment, the system may also include a first multiscale wick on a first interior wall of the enclosure, and may include a heater blanket disposed on an exterior wall of the enclosure, the exterior wall on an opposite side of the first interior wall. A second multiscale wick may also be included on a second interior wall of the enclosure that opposes the first interior wall. The heat source may be an energy storage device that is one of a first plurality of energy storage devices disposed within the enclosure. The first plurality of energy storage devices may be stacked in a mono-block configuration on the first multiscale wick structure, and each of the first plurality of energy storage devices may have an outer surface substantially encompassed by a respective one of a plurality of woven ceramic wicks. The system may also include a secondary multiscale wick extending along the plurality of woven ceramic wicks, the secondary multiscale wick in liquid communication with the plurality of woven ceramic wicks. The secondary multiscale wick may extend along a radius R of each of the plurality of woven ceramic multiscale wicks to increase a surface area of liquid contact between the secondary multiscale wick and each of the plurality of woven ceramic multiscale wicks. In other embodiments, the system may include a second plurality of heat sources stacked in the mono-block configuration on the first multiscale wick structure, the second plurality of heat sources each having an outer surface substantially encompassed by a respective one of a plurality of woven ceramic multiscale wicks. An interior frame structure may be provided between the first and second pluralities of stacked heat sources.
Another system for thermal management and structural containment has an enclosure, a battery disposed within the enclosure, a woven ceramic jacket encompassing at least a portion of an outer surface of the battery, and a working fluid in liquid communication with the woven ceramic jacket. The system may also have a first multiscale wick structure on an interior side of a first wall of the enclosure, and a heater disposed on an exterior side of the first wall, the heater disposed in complementary opposition to the first multiscale wick structure. The battery may be one of a first plurality of batteries disposed within the enclosure. The first plurality of batteries may be stacked in a mono-block configuration, and, in one embodiment, such batteries may also be stacked on an interior base wick. The system may also include a second plurality of batteries stacked in the mono-block configuration on the interior base wick, the second plurality of batteries each having an outer surface encompassed by a respective one of a plurality of woven ceramic jackets. An interior frame structure may also be provided between the first and second pluralities of stacked batteries.
A method of transferring heat includes receiving thermal energy in a multiscale wick substantially encompassing an outer surface of a battery in an enclosure, and transferring thermal energy between the multiscale wick and a first multiscale wick structure on an interior side of a first wall of the enclosure. The method may also include generating vapor in the multiscale wick in response to receipt of the thermal energy, and generating condensate in the first multiscale wick structure. In one embodiment, heat is transferred from the battery to the multiscale wick. In some embodiments, the method may also include providing structural reinforcement against radial expansion of the battery by the multiscale wick. In one embodiment of the method referred to as “reverse operation,” the method may include generating vapor in the first multiscale wick structure on the interior side of the first wall of the enclosure in response to receipt of the thermal energy and generating condensate in the multiscale wick that substantially encompasses the outer surface of the battery so that heat may be transferred from the multiscale wick to the battery.
The components in the figures are not necessarily to scale, emphasis instead being placed upon illustrating the principals of the invention. Like reference numerals designate corresponding parts throughout the different views.
A system is disclosed that provides a single unique solution for both thermal management and failure containment of heat sources such as batteries. Under normal operating conditions, the system acts as a liquid-to-vapor phase change thermal management system. Under fault conditions, the system behaves as a firewall and a failure containment system.
Interior wick structures 125 may be disposed on pairs of opposing interior walls (130, 135), with each interior wick structure 125 in liquid communication with the interior base wick 115 on the bottom of the enclosure 120 to transport liquid using a wicking action between them. Each wick 105, bottom wick (not shown), interior base wick 115, and the interior wick structures 125 are preferably electrically non-conductive and capable of withstanding temperatures in excess of 1000° C. Although the heat sources are illustrated as seated in a bottom portion of the enclosed heat chamber, the heat sources may be seated on one of the walls of the opposing pairs of interior walls (130, 135) or may span the width or height of the enclosure. The opposing pairs of interior walls (130, 135) may be formed of a heat conducting material such as metal to receive excess heat from the interior wick structure 125. The enclosure 120 may be charged with a working fluid that is preferably a dielectric liquid, such as 3M NOVEC 7200, that has a freeze point of −138° C., boiling point of 76° C. (at 1 atm. pressure) and a critical temperature of ˜170° C. thus enabling a typical battery operating range of −40 to +70° C. The saturation pressure may be slightly below 1 atm. when the ambient temperature (outside battery box) is 70° C. In embodiments where the enclosure is not cuboid, such as an enclosure in the form of a sphere or cylinder, “pairs of opposing interior walls” may refer to wall segments on opposite sides of the enclosure from one another.
In a preferred embodiment, the battery 100 may have a substantial portion of its outer surface encompassed by a multiscale wick 200 that may be formed of high temperature materials such as ceramic (alternatively referred to as a “ceramic jacket” or “ceramic multiscale wick”) or glass fibers. As used herein, the phrase “multiscale wick” may refer to a wick structure that has different average pore sizes and distribution to provide multiple effective pore sizes for capillary pumping. Examples of multiscale wicks may include a single-layer wick having fibers of different diameters that are stacked (i.e., more than one fiber deep) or sprayed onto a surface; a plurality of layers of fibers, with each adjacent layer having a different pore size distribution (see
During operation, as used in the enclosure 120 of
Liquid communication between and among the primary jackets 405 is enhanced by liquid communication along the secondary jacket 410. Conforming the secondary jacket 410 shape to the shape of each primary jacket 405 may enhance such liquid communication. For example, rather than forming the secondary jacket in a plane having flat exterior surfaces, the secondary jacket 410 may extend along a partial radius R of each respective woven ceramic jacket 405 that encompasses the outer cylindrical surface of each battery cell 100. (See
In an alternative use of the mono-block 400, the primary and secondary jackets (405, 410) may receive heat energy in the form of vapor from locations removed from the mono-block 400. The vapor may condense on the secondary jacket 410, and/or through the secondary jacket 410 to the primary jacket 405, for communication of the condensed liquid by wicking action to the batteries 100. In this manner, the batteries may receive excess heat energy through the primary and secondary jackets (405, 410) rather than expelling excess heat energy from the batteries 100 as described above. This method may be useful for warming batteries 100 for use in climates that would otherwise be too cold for ideal operation at startup. As the batteries 100 are used and begin to generate their own excess heat, the transfer of heat energy between the batteries 100 and locations removed from the mono-block may be reversed, with vapor created on the outer surface of the batteries 100.
Each mono-block has complementary panels (630, 635) spaced apart at a distance that approximates the length of the batteries 100 to facilitate electrical connection between battery terminals on the batteries and terminals on the complementary panels (630, 635). Through suitable electrical connection between the complementary panels, positive terminals of a first mono-block may be connected to negative terminals of a second mono-block for suitable electrical configuration.
Cooling capability in excess of 100 W/cm2 can be achieved by designing the multiscale pores (10 nm to 1 mm) of the primary and secondary cell jackets (705, 710). The cooling capability may far exceed the typical power dissipation density of a cell 720 even under the most severe discharge rate condition of 30 C (i.e., 30 times faster than the rated capacity of the cell or battery). Due to the connected vapor space within the battery case 700 and the identical vapor saturation temperature, a nearly isothermal condition can be achieved among cells 720 inside a large battery module 710, even with different heat dissipation between the cells 720. A small overpressure gas release valve may be added for safety.
Dielectric liquid, such as 3M NOVEC 7200 has a freeze point of −138° C., boiling point of 76° C. (at 1 atm. pressure) and a critical temperature of ˜170° C. Thus it is suitable for the entire ambient temperature range under which the battery 700 may operate (−40 to +70° C.). The saturation pressure is slightly below 1 atm. when the ambient temperature (outside the battery box 715) is 70° C. The small pressure differential eases the strength and thickness requirements of the battery box wall 725, resulting in a lightweight battery with effective heat conduction through the wall 725. The battery preferably sealed to accomplish the operation described above, similar to current lead acid batteries. A gas release valve can provide a vapor escape path in case of overpressure if the system is overheated.
In another embodiment described for convenience as “reverse operation,” thermal energy is received in the primary jacket of the battery by means of vapor generated in a first multiscale wick on an interior side of a first wall of the enclosure (block 915). The vapor in the first multiscale wick may be created from a liquid-to-vapor phase change prompted by thermal energy received from a heat source exterior to the enclosure or from a heat source mounted to an exterior of the enclosure for communication to the primary jacket. In one embodiment, the heat source is a heater blanket. The vapor-to-liquid phase change in the primary jacket (block 920) serves to warm the battery for its use in environments that would otherwise be too cold for ideal operation of the battery at startup. In this “reverse operation” mode, working fluid in the suspended form of vapor is in communication with the primary jacket for the vapor-to-liquid phase change heat transfer operation.
In forward operation, the vapor generated in the primary jacket (block 905) is transferred to the first multiscale wick on the interior side of the first wall of the enclosure (block 925). The vapor may undergo a vapor-to-liquid phase change as it is cooled by the first multiscale wick to form condensate (block 930) to finally draw the excess heat energy away from the battery. The condensate may then be wicked or otherwise transported back to the primary jacket for receipt of additional thermal energy to accomplish a liquid-to-vapor phase change for transport of excess heat energy from the battery back to the first multiscale wick for transport of the thermal energy out of the enclosure.
A rechargeable lithium iron phosphate (LFP) battery, cylindrical in shape with nominal dimensions 26 mm in diameter and 65 mm in height (26650 LFP, K2 Energy) is placed inside a vapor-tight enclosure. Electrical leads are connected to the cell using feedthroughs in the cover of the enclosure. Certain amount of dielectric liquid 3M NOVEC 7200 is placed at the bottom of the enclosure. The battery is first charged at 0.5 C rate to 3.65 V and then further charged at constant voltage with the current decreasing over time down to 65 mA. The battery is then discharged fully to 0% SOC under a constant resistance load, starting with 10 Amp current. The temperature of the cell is recorded as a function of time during the discharge. The ambient temperature around the enclosure is kept at 40° C. The temperature of the cell wall is rising as shown in
A cylindrical rechargeable 26650 LFP cell (26650, K2 Energy) is covered using 250 microns thick non-woven porous structure on the cylindrical cell wall and placed inside a vapor-tight enclosure. The charge and discharge process of example 1 is repeated. The temperature rise during the discharge is shown in
The experiment in example 1 is repeated except that the charge is carried at a constant current (CC) 4 Amp (1.5 C) charge until cell voltage reaches 3.65 V (approximately at ˜3000 s), and then constant voltage charge until current trickles down 65 mA. The ambient temperature is 60° C. The temperature of the cell is recorded as a function of time during the charge and the temperature peaks just after the constant current step at 11° C., as shown in
The cell is covered with a non-woven porous structure as in example 2 and the charge procedure of example 3 is followed. In this example, the temperature increase of the cell peaks at ˜2° C. (
While various implementations of the application have been described, it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible that are within the scope of this invention.
Bhunia, Avijit, Cai, Qingjun, Sudre, Olivier
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